Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 1276M30G02, which you have taken interest in. This Case Turbine Aircraft Gas Turbin item is listed alongside the NSN 2840-01-447-2846 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 1276M30G02 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-447-2846 part number 1276M30G02 today, knowing we will support all your operational needs with care.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-447-2846 Item PartTypeName: CASE,TURBINE,AIRCRAFT GAS TURBIN | 2840 | 014472846 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
KDS 2840-4003 | 1 | 1 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 2.359 INCHES MINIMUM AND 2.383 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG F110GE129 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ AND FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | COVER,COOLING AIR-HIGH PRESSURE TURBINE NOZZLE,OUTER |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
FEAT | SPECIAL FEATURES | USED ON THE NOZZLE ASSEMBLY AND SEGMENTS, SEALS AND SUPPORTS |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-14, FIG 74, IND 17 |
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